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A 737-300/400/500MAINTENANCE MANUAL
C95215
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A 737-300/400/500MAINTENANCE MANUAL
C95218
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A
737-300/400/500MAINTENANCE MANUAL
(3) The FMC is packaged in accordance with ARINC 600. The basic chassis is composed of aluminum extrusions and plates, mainly secured by epoxy, to form a homogeneous box with two open sides. One side of the FMC is closed by use of a cover attached with quick-disconnect fasteners. The power supply assembly forms the other side cover and is held in place by captive machine screws. There is no internal fan, as the FMC receives its cooling air from the airplane air-conditioning system. The cover and power supply must be fastened in place for proper unit cooling.
B. Control Display Unit (CDU)
(1)
The CDU includes a display and keyboard that allows the operator to interface with the FMC. The CDU displays airplane initialization, reference, flight planning, and performance data. The CDU keyboard enables the operator to enter parameter values to support processing of flight management functions.
(2)
The CDU also provides a means of initiating, controlling, and displaying the operation and status of BITE, for the flight management system.
(3)
The CDU assembly contains the following components: a keyboard lightplate assembly, chassis, high and low voltage power supplies, circuit cards, and a Cathode Ray Tube (CRT).
(4)
The front panel on the CDU contains the keyboard switches with integral lighting. The CDU keys are shaped to help set apart their respective functions. The numeric keys are circular in shape, while the alphabetical keys are square. The line select and function keys are rectangular in form.
(5)
The CDU chassis contains the high and low voltage power supplies. The chassis consists of multiple plates that form a rigid EMI-tight enclosure.
(6)
The CRT subassembly contains a five-inch cathode ray tube, yoke, high contrast filter, and an EMI shield. The cathode ray tube is flat faced; a glass optical filter is bonded to the front of the tube.
C. Digital - Analog Adapter (DAA)
(1) Sensors with analog outputs, and displays with analog inputs, must be able to communicate with the digital FMC. Conversion of analog signals to digital signals, and vice versa, is accomplished by the DAA.
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D.
E.
F.
G.
H.
I.
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737-300/400/500MAINTENANCE MANUAL
Distance Measuring Equipment (DME)
(1)
The DME interrogators provide distance information to the FMC, through the DAA. When manual tuning is selected on the VHF navigation control panel, a manually selected DME frequency is tuned. If automatic tuning is selected the DME interrogators are tuned by signals from the FMC.
(2)
When automatic tuning is selected, station selection is determined by the FMC, using navigation information and station geometry information. In the event that one of the DME interrogators is manually tuned to a station that does not satisfy the range and geometry of the FMC, (or if one of the DME interrogators fail); the FMC will automatically place the remaining DME interrogator in a frequency agility mode, provided automatic tuning has been selected. This remaining DME interrogator will be automatically tuned, (at five-second intervals), between two DME stations. Two DME stations, however, must be available that satisfy the range and geometry criteria of the FMC. Agility tuning allows DME/DME position determination with a single DME.
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